Abstract
The effect of interaction between combustion processes and structural deformation of solid propellant was considered. The combustion analysis was performed on the basis of deformed crack geometry, which was determined from the structural analysis. On the other hand, input data for the structural analysis, such as press distribution along the crack boundary and ablation velocity of the crack, were determined from the combustion analysis.
| Original language | English |
|---|---|
| Pages (from-to) | 67-90 |
| Number of pages | 24 |
| Journal | NASA Conference Publication |
| Publication status | Published - 1980 |
| Event | NASA Conf Publ CP 2147, Res In Nonlinear Struct and Solid Mech - Washington, DC, USA Duration: 6 Oct 1980 → 8 Oct 1980 |